Invention Grant
- Patent Title: Cooled component for a gas turbine engine
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Application No.: US16751494Application Date: 2020-01-24
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Publication No.: US11326518B2Publication Date: 2022-05-10
- Inventor: Maleek E. Wedderburn , Nurhak Erbas-Sen , John W. Mubeezi , Fumitaka Ichihashi , Roger O. Coffey
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Farmington
- Agency: Carlson, Gaskey & Olds, P.C.
- Main IPC: F02C7/12
- IPC: F02C7/12 ; F01D9/02

Abstract:
A combustor panel arrangement for a gas turbine engine. The combustor panel arrangement includes a first combustor panel that has a first edge. A second combustor panel has a second edge facing the first edge. A first plurality of effusion holes extend through the first edge towards the second edge along a corresponding one of a first plurality of flow paths. A second plurality of effusion holes extend through the second edge along a corresponding one of a second plurality flow paths towards the first edge. The first plurality of flow paths and the second plurality of flow paths are non-intersecting.
Public/Granted literature
- US20200256250A1 COOLED COMPONENT FOR A GAS TURBINE ENGINE Public/Granted day:2020-08-13
Information query
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